EP1926008B1 - Gas pressure reducer - Google Patents

Gas pressure reducer Download PDF

Info

Publication number
EP1926008B1
EP1926008B1 EP07103884A EP07103884A EP1926008B1 EP 1926008 B1 EP1926008 B1 EP 1926008B1 EP 07103884 A EP07103884 A EP 07103884A EP 07103884 A EP07103884 A EP 07103884A EP 1926008 B1 EP1926008 B1 EP 1926008B1
Authority
EP
European Patent Office
Prior art keywords
jacket
slider
pressure reducer
gas
designed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP07103884A
Other languages
German (de)
French (fr)
Other versions
EP1926008A3 (en
EP1926008A2 (en
Inventor
Lucio Notaro
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Metatron SpA
Original Assignee
Metatron SpA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Metatron SpA filed Critical Metatron SpA
Publication of EP1926008A2 publication Critical patent/EP1926008A2/en
Publication of EP1926008A3 publication Critical patent/EP1926008A3/en
Application granted granted Critical
Publication of EP1926008B1 publication Critical patent/EP1926008B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D16/00Control of fluid pressure
    • G05D16/04Control of fluid pressure without auxiliary power
    • G05D16/10Control of fluid pressure without auxiliary power the sensing element being a piston or plunger
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/023Valves; Pressure or flow regulators in the fuel supply or return system
    • F02M21/0233Details of actuators therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/023Valves; Pressure or flow regulators in the fuel supply or return system
    • F02M21/0239Pressure or flow regulators therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D19/00Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D19/02Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with gaseous fuels
    • F02D19/026Measuring or estimating parameters related to the fuel supply system
    • F02D19/027Determining the fuel pressure, temperature or volume flow, the fuel tank fill level or a valve position
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels

Definitions

  • the present invention relates to a gas pressure reducer.
  • the present invention relates to a pressure reducer which can be used in gas supply systems for internal combustion engines.
  • These gas supply systems usually comprise a pressurised gas tank, a plurality of pipes connecting the gas tank to the engine and a pressure reducer which reduces the pressure of the gas in the tank to a pressure suitable for supplying it to the engine and therefore compatible with combustion parameters.
  • the pressure of the gas in the tank is usually between 200 and 15 bar.
  • the pressure for supplying the gas to the engine must be kept at a substantially constant predetermined value.
  • the reducer advantageously comprises a single reduction chamber, being much more compact than earlier reducers which had a plurality of reduction stages and a reduction chamber for each stage.
  • the above-mentioned single chamber is basically formed by the presence of a movable shutter, or slider, in a respective jacket.
  • the shutter is subject to the opposing action of an elastic element, usually a helical spring, which has a first end coil in contact with the shutter whilst the second end coil, longitudinally opposite the first, engages a ring-shaped inner wall of the jacket.
  • a first, rough calibration of the reducer is provided by selecting the spring which engages with the movable shutter whilst, for precision calibration, work is required inside the jacket, inserting or removing suitable spacers between the second coil and the ring-shaped wall of the jacket.
  • Document US 5899221 discloses a fluid pressure regulator capable of adjustably setting a cut-off pressure between an upper and a lower limit.
  • the regulator has a two-piece valve body where the two pieces are threadably joined such that adjusting the distance between the two pieces of the valve body.
  • Document US 5419365 shows a regulator for high pressure water blast system including a body which houses a replaceable valve cartridge that includes a tubular seat member and an axially slidable valve element.
  • the seat member is hydraulically biased against a stop shoulder and the valve element is hydraulically biased towards an adjusting knob.
  • the aim of the present invention is to provide a pressure reducer which allows practical and rapid calibration and at the same time is simple and economical to make.
  • the numeral 1 denotes as a whole the pressure reducer in accordance with the present invention.
  • the reducer 1 comprises a central containment body 2 inside which there extends a pipe 3 through which the gas passes and a compensation chamber 4.
  • the pipe 3 comprises a first, inlet stretch 5 and a second, outlet stretch 6 for the gas, operatively connected to one another by the compensation chamber 4.
  • the first, inlet stretch 5 of the pipe 3 has a mouth 7 designed to be fluidly connected with a tank, not illustrated, used to store the gas and an end portion 5a, giving onto the compensation chamber 4, the portion 5a substantially extending along a predetermined direction D and having a first narrowing 8.
  • a solenoid valve 9 Acting on the end portion 5a of the first, inlet stretch 5 there is a solenoid valve 9, of the known type, which connects the gas tank with the reducer 1 when the internal combustion engine is on.
  • the solenoid valve interrupts that connection when the engine is switched off. Therefore, the solenoid valve 9 substantially has a safety function, to prevent the pressure of the gas contained in the tank and in the first stretch 5 of the pipe 3 from continuously acting on the reducer 1 seals.
  • the reducer 1 also comprises, positioned along the first stretch 5 of the pipe 3, a filter 10 designed to catch the impurities present in the gas entering the reducer 1.
  • the reducer 1 also comprises a sensor 11 for detecting the pressure of the gas entering the reducer 1, the sensor 11 being connected to the pipe 3 upstream of the filter 10 on the path P followed by the gas passing through the body 2.
  • the sensor 11 can detect, apart from negligible pressure losses in the pipe, not illustrated, connecting the gas tank and the reducer 1, the pressure value in the tank itself and, from that value, therefore arrive at the quantity of gas present in the tank.
  • a hot fluid for example the engine coolant, is introduced into said heating pipes 12 so as to counteract the significant reduction in temperature to which the gas is subjected after it has expanded.
  • the compensation chamber 4 extends below the end portion 5a of the inlet stretch 5 and is formed by the containment body 2 together with a slider 13.
  • the slider 13 can move both ways in direction D which therefore forms a direction of sliding for the slider 13.
  • the slider 13 has an active portion 14 which, together with the end portion 5a of the first, inlet stretch 5, forms a second narrowing 15 of the gas pipe 3.
  • the slider 13 comprises a ring-shaped flange 16 which substantially extends perpendicular to the predetermined direction D of sliding of the slider 13.
  • the slider 13 is housed in and supported by a cylindrical jacket 17 which extends longitudinally according to the predetermined direction D.
  • the cylindrical jacket 17 has a first cylindrical inner wall 17a on which the ring-shaped flange 16 slidably engages, and a second cylindrical inner wall 17b, coaxial with the first and having a smaller diameter, on which the slider 13 slidably engages with a stretch close to the active portion 14.
  • the cylindrical jacket 17 is connected to the central containment body 2 in a sealed fashion by a screw connection 18.
  • an axially symmetrical cavity 19 having a base wall 19a which partly delimits the top of the compensation chamber 4.
  • the axially symmetrical cavity 19 also comprises an internally threaded cylindrical surface 20 on which a corresponding externally threaded cylindrical portion 21 of the jacket 17 engages with a screwing action.
  • the jacket 17 comprises an end zone 22 extending from the threaded cylindrical portion 21 towards the base wall 19a and giving onto the second narrowing 15.
  • the jacket 17 comprises a circumferential groove 23 for housing a ring-shaped gas seal 24.
  • the ring-shaped seal 24 engages with a cylindrical inner wall of the cavity 19 to provide a gasproof seal preventing unwanted gas leaks through the screw connection 18.
  • a grub screw 26 is inserted and screwed in the hole 25, being designed to engage with one end in contact with the cylindrical portion 21 of the jacket 17.
  • the grub screw 26 engages the threaded cylindrical portion of the cylindrical jacket 17, it prevents rotation of the jacket 17 relative to the central body 2.
  • a predetermined position of the active portion 14 of the slider 13 relative to the second narrowing 15 is fixed.
  • the slider 13 is supported by the jacket 17 and therefore having defined a fixed position for the jacket 17 relative to the body 2 is the equivalent of defining a fixed position for the slider 13, obviously apart from the possible movements of the slider along the direction D, movements due to the variation in the pressure of the gas passing through the pipe 3.
  • the grub screw 26 forms, for the jacket 17, locking means 27 designed to prevent its screwing and/or unscrewing rotation relative to the central body 2.
  • the locking means 27 comprise, in place of or in addition to the grub screw 26, a threaded locking ring, also not illustrated, screwed on the threaded cylindrical portion 21 of the cylindrical jacket 17 and designed to tighten against a second outer wall 2b of the body 2, said wall visible in Figure 2 .
  • the locking ring acts as a tightening lock nut.
  • the reducer 1 also comprises, supported by the jacket 17, a relief valve 30, of the known type and therefore not described in detail, designed to prevent the pressure in the chamber 4 from exceeding predetermined safety values for any reason.
  • the possibility of adjusting the position of the active portion 14 of the slider 13 relative to the end portion 5a of the first stretch 5 therefore constitutes a means of adjusting the pressure of the gas downstream of the second narrowing 15, that is to say, in other words, the pressure of the gas supplied to the internal combustion engine, not illustrated.
  • the pressure of the gas at the reducer 1 outlet is adjusted in a practical and effective way by simply rotating a part of the reducer 1, without having to disassemble any reducer part or component.
  • the engagement zone 28 consists of a flattened portion 29 of the cylindrical outer wall of the jacket 17.

Abstract

The gas pressure reducer (1) comprises a central body (2), a pipe (3) through which the gas passes, made in the central body (2), the pipe (3) having a first narrowing (8) designed to produce a fall in the gas pressure, a slider (13) able to move along a predetermined direction (D) and having an active portion (14) forming a second narrowing (15) in the pipe (3), a jacket (17) for housing and supporting the slider (13).

Description

  • The present invention relates to a gas pressure reducer.
  • In particular, the present invention relates to a pressure reducer which can be used in gas supply systems for internal combustion engines.
  • Economic advantages and limited pollution are achieved by applying systems which supply gas such as methane or liquid petroleum gas (LPG) on internal combustion engines, both fixed and for vehicle drive.
  • These gas supply systems usually comprise a pressurised gas tank, a plurality of pipes connecting the gas tank to the engine and a pressure reducer which reduces the pressure of the gas in the tank to a pressure suitable for supplying it to the engine and therefore compatible with combustion parameters.
  • Depending on how full the tank is, the pressure of the gas in the tank is usually between 200 and 15 bar. In contrast, the pressure for supplying the gas to the engine must be kept at a substantially constant predetermined value.
  • According to another prior solution by the Applicant, the reducer advantageously comprises a single reduction chamber, being much more compact than earlier reducers which had a plurality of reduction stages and a reduction chamber for each stage.
  • Said solution, although having many advantageous aspects, may be improved in terms of efficiency and practical use.
  • The above-mentioned single chamber is basically formed by the presence of a movable shutter, or slider, in a respective jacket. The shutter is subject to the opposing action of an elastic element, usually a helical spring, which has a first end coil in contact with the shutter whilst the second end coil, longitudinally opposite the first, engages a ring-shaped inner wall of the jacket.
  • A first, rough calibration of the reducer is provided by selecting the spring which engages with the movable shutter whilst, for precision calibration, work is required inside the jacket, inserting or removing suitable spacers between the second coil and the ring-shaped wall of the jacket.
  • The fact that precision calibration is basically done inside the jacket implies that many of the reducer's components, including the jacket, the shutter and the spring, must be disassembled then reassembled.
  • Even if this is done by specialised, expert personnel, inevitably the above-mentioned pressure reducer calibration as a whole ties up a significant amount of time and resources.
  • Document US 5899221 discloses a fluid pressure regulator capable of adjustably setting a cut-off pressure between an upper and a lower limit. The regulator has a two-piece valve body where the two pieces are threadably joined such that adjusting the distance between the two pieces of the valve body.
  • Document US 5419365 shows a regulator for high pressure water blast system including a body which houses a replaceable valve cartridge that includes a tubular seat member and an axially slidable valve element. The seat member is hydraulically biased against a stop shoulder and the valve element is hydraulically biased towards an adjusting knob.
  • The aim of the present invention is to provide a pressure reducer which allows practical and rapid calibration and at the same time is simple and economical to make.
  • The technical features of the invention, with reference to the above aims, are clearly described in the claims below and its advantages are more apparent from the detailed description which follows, with reference to the accompanying drawings which a illustrate preferred embodiment of the invention provided merely by way of example without restricting the scope of the inventive concept, and in which:
    • Figure 1 is a perspective top view of a pressure reducer in accordance with the present invention;
    • Figure 2 is a cross-section of the pressure reducer of Figure 1.
  • As illustrated in the accompanying drawings, the numeral 1 denotes as a whole the pressure reducer in accordance with the present invention.
  • With reference to Figure 2, the reducer 1 comprises a central containment body 2 inside which there extends a pipe 3 through which the gas passes and a compensation chamber 4.
  • The gas, as it passes through the pipe 3, moves forward along a path P shown with a dashed line in Figure 1.
  • The pipe 3 comprises a first, inlet stretch 5 and a second, outlet stretch 6 for the gas, operatively connected to one another by the compensation chamber 4.
  • The first, inlet stretch 5 of the pipe 3 has a mouth 7 designed to be fluidly connected with a tank, not illustrated, used to store the gas and an end portion 5a, giving onto the compensation chamber 4, the portion 5a substantially extending along a predetermined direction D and having a first narrowing 8.
  • Acting on the end portion 5a of the first, inlet stretch 5 there is a solenoid valve 9, of the known type, which connects the gas tank with the reducer 1 when the internal combustion engine is on. The solenoid valve interrupts that connection when the engine is switched off. Therefore, the solenoid valve 9 substantially has a safety function, to prevent the pressure of the gas contained in the tank and in the first stretch 5 of the pipe 3 from continuously acting on the reducer 1 seals.
  • In Figure 2 the solenoid valve 9 is illustrated in a configuration which opens the pipe 3, this configuration therefore being assumed when the internal combustion engine is on.
  • The reducer 1 also comprises, positioned along the first stretch 5 of the pipe 3, a filter 10 designed to catch the impurities present in the gas entering the reducer 1.
  • The reducer 1 also comprises a sensor 11 for detecting the pressure of the gas entering the reducer 1, the sensor 11 being connected to the pipe 3 upstream of the filter 10 on the path P followed by the gas passing through the body 2.
  • With this arrangement, the sensor 11 can detect, apart from negligible pressure losses in the pipe, not illustrated, connecting the gas tank and the reducer 1, the pressure value in the tank itself and, from that value, therefore arrive at the quantity of gas present in the tank.
  • In the central containment body 2 there is a pair of heating pipes, labelled 12. A hot fluid, for example the engine coolant, is introduced into said heating pipes 12 so as to counteract the significant reduction in temperature to which the gas is subjected after it has expanded.
  • Again with reference to Figure 2, the compensation chamber 4 extends below the end portion 5a of the inlet stretch 5 and is formed by the containment body 2 together with a slider 13.
  • The slider 13 can move both ways in direction D which therefore forms a direction of sliding for the slider 13.
  • As shown in Figure 2, at an upper end zone 13a, the slider 13 has an active portion 14 which, together with the end portion 5a of the first, inlet stretch 5, forms a second narrowing 15 of the gas pipe 3.
  • When the slider 13 moves along the direction D in a first direction, indicated by the arrow F1 in Figure 2, the active portion 14 moves away from the end portion 5a of the inlet stretch 5 and, consequently, the dimensions of the second narrowing 15 increase, that is to say, the area of the cross-section for the passage of the gas flow at that point increases.
  • On the other hand, when the slider 13 moves in a second direction, indicated by the arrow F2, towards the end portion 5a of the inlet stretch 5, the dimensions of the second narrowing 15 are reduced.
  • Again with reference to Figure 1, the slider 13 comprises a ring-shaped flange 16 which substantially extends perpendicular to the predetermined direction D of sliding of the slider 13.
  • The slider 13 is housed in and supported by a cylindrical jacket 17 which extends longitudinally according to the predetermined direction D.
  • The cylindrical jacket 17 has a first cylindrical inner wall 17a on which the ring-shaped flange 16 slidably engages, and a second cylindrical inner wall 17b, coaxial with the first and having a smaller diameter, on which the slider 13 slidably engages with a stretch close to the active portion 14.
  • The cylindrical jacket 17 is connected to the central containment body 2 in a sealed fashion by a screw connection 18.
  • In detail, in the body 2 there is an axially symmetrical cavity 19 having a base wall 19a which partly delimits the top of the compensation chamber 4. The axially symmetrical cavity 19 also comprises an internally threaded cylindrical surface 20 on which a corresponding externally threaded cylindrical portion 21 of the jacket 17 engages with a screwing action.
  • Again with reference to Figure 2, the jacket 17 comprises an end zone 22 extending from the threaded cylindrical portion 21 towards the base wall 19a and giving onto the second narrowing 15.
  • At the end zone 22, the jacket 17 comprises a circumferential groove 23 for housing a ring-shaped gas seal 24. In particular, when the jacket 17 is at least partly inserted in the axially symmetrical cavity 19, the ring-shaped seal 24 engages with a cylindrical inner wall of the cavity 19 to provide a gasproof seal preventing unwanted gas leaks through the screw connection 18.
  • As illustrated in Figure 1, in a first outer wall 2a of the body 2 there is a threaded through-hole 25 opening into the cavity 19, at its threaded cylindrical surface 20.
  • A grub screw 26 is inserted and screwed in the hole 25, being designed to engage with one end in contact with the cylindrical portion 21 of the jacket 17.
  • When, after being screwed in the hole 25, the grub screw 26 engages the threaded cylindrical portion of the cylindrical jacket 17, it prevents rotation of the jacket 17 relative to the central body 2.
  • In this way, a predetermined position of the active portion 14 of the slider 13 relative to the second narrowing 15 is fixed. The slider 13 is supported by the jacket 17 and therefore having defined a fixed position for the jacket 17 relative to the body 2 is the equivalent of defining a fixed position for the slider 13, obviously apart from the possible movements of the slider along the direction D, movements due to the variation in the pressure of the gas passing through the pipe 3.
  • The grub screw 26 forms, for the jacket 17, locking means 27 designed to prevent its screwing and/or unscrewing rotation relative to the central body 2.
  • According to an alternative embodiment of the invention, not illustrated, the locking means 27 comprise, in place of or in addition to the grub screw 26, a threaded locking ring, also not illustrated, screwed on the threaded cylindrical portion 21 of the cylindrical jacket 17 and designed to tighten against a second outer wall 2b of the body 2, said wall visible in Figure 2. Basically, the locking ring, not illustrated, acts as a tightening lock nut.
  • The reducer 1 also comprises, supported by the jacket 17, a relief valve 30, of the known type and therefore not described in detail, designed to prevent the pressure in the chamber 4 from exceeding predetermined safety values for any reason.
  • In practice, as illustrated in Figure 2, the active portion 14 of the slider 13, together with the end portion 5a of the first stretch 5, as already indicated, forms the second narrowing 15 of the gas pipe 3. Since at said second narrowing 15 the gas expands and its pressure is simultaneously reduced, obviously the size of that narrowing 15 affects the pressure of the gas in the compensation chamber 4 and downstream of it, relative to the gas supply path P.
  • The possibility of adjusting the position of the active portion 14 of the slider 13 relative to the end portion 5a of the first stretch 5 therefore constitutes a means of adjusting the pressure of the gas downstream of the second narrowing 15, that is to say, in other words, the pressure of the gas supplied to the internal combustion engine, not illustrated.
  • Again with reference to Figure 2, by rotating the cylindrical jacket 17 about its own axis coinciding with the direction D, since the jacket 17 engages with the body 2 by means of a screwing action, a rotation of the jacket 17 corresponds to a jacket movement along the direction D. The relationship between the angle of rotation and forward movement clearly depends on the thread used for the screw connection 18.
  • Basically, by screwing and unscrewing the jacket 17 relative to the body 2, it is possible to continuously change the position of the active part of the slider relative to the end portion 5a and therefore to change the size of the second narrowing 15. This consequently changes the pressure of the gas which flows into the compensation chamber 4 and is then supplied to the internal combustion engine.
  • Advantageously, with the present invention, the pressure of the gas at the reducer 1 outlet is adjusted in a practical and effective way by simply rotating a part of the reducer 1, without having to disassemble any reducer part or component.
  • Advantageously, as illustrated in Figure 1, on the cylindrical outer wall of the jacket 17 there are one or more zones 28 for engaging with a tool, not illustrated, such as a spanner, for precision rotation of the jacket 17.
  • In the embodiment illustrated, the engagement zone 28 consists of a flattened portion 29 of the cylindrical outer wall of the jacket 17.

Claims (7)

  1. A gas pressure reducer comprising:
    - a central body (2);
    - a pipe (3) through which the gas passes, made in the central body (2), the pipe (3) having a first narrowing (8) designed to produce a fall in the gas pressure;
    - a slider (13) able to move along a predetermined direction (D) and having an active portion (14) forming a second narrowing (15) in the pipe (3);
    - a jacket (17) for housing and supporting the slider (13), the jacket (17) being connected to the central body (2) by a screw connection (18), in such a way that by screwing or unscrewing the jacket (17) relative to the body (2), the active portion (14) of the slider (13) housed in the jacket (17) is moved towards or, respectively, away from the body (2), varying the size of the second narrowing (15);
    the cylindrical jacket (17) having a first cylindrical inner wall (17a) on which a ring-shaped flange (16) of the slider (13) slidably engages, and a second cylindrical inner wall (17b), coaxial with the first and having a smaller diameter, on which the slider (13) slidably engages with a stretch close to the active portion (14);
    the gas pressure reducer being characterised in that the first inner wall (17a) and the second inner wall (17b) are realised in a single body.
  2. The pressure reducer according to claim 1, characterised in that the jacket (17) comprises a threaded cylindrical portion (21) designed to engage with a screwing action on a respective internally threaded cylindrical surface (20) in the body (2).
  3. The pressure reducer according to claim 2, characterised in that, at an end zone (22) designed to give onto the second narrowing (15), the jacket (17) comprises a circumferential groove (23) for housing a ring-shaped gas seal (24).
  4. The pressure reducer according to any of the claims from 1 to 3, characterised in that it comprises jacket (17) locking means (27), said means (27) being designed to prevent jacket (17) screwing or unscrewing rotation on the body (2) when a desired slider (13) active portion (14) position has been reached relative to the body (2).
  5. The pressure reducer according to claim 4, characterised in that the locking means (27) comprise a threaded grub screw (26) inserted in a respective through-hole (25) made in the body (2), the grub screw (26) being designed to engage the jacket (17).
  6. The pressure reducer according to claim 4, characterised in that the locking means comprise a threaded locking ring, screwed on said threaded cylindrical portion (21) of the jacket (17) and designed to tighten against an outer wall of the body (2).
  7. The pressure reducer according to any of the claims from 1 to 6, characterised in that the jacket (17) comprises at least one zone (28) for engaging with a tool for rotating the jacket (17) relative to the body (2).
EP07103884A 2006-11-27 2007-03-09 Gas pressure reducer Active EP1926008B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT000099U ITBO20060099U1 (en) 2006-11-27 2006-11-27 PRESSURE REDUCER FOR GAS.

Publications (3)

Publication Number Publication Date
EP1926008A2 EP1926008A2 (en) 2008-05-28
EP1926008A3 EP1926008A3 (en) 2009-09-23
EP1926008B1 true EP1926008B1 (en) 2011-05-11

Family

ID=39016425

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07103884A Active EP1926008B1 (en) 2006-11-27 2007-03-09 Gas pressure reducer

Country Status (3)

Country Link
EP (1) EP1926008B1 (en)
AT (1) ATE509306T1 (en)
IT (1) ITBO20060099U1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2013129455A (en) * 2010-12-21 2015-01-27 ЭМЕР С.п.А. EVAPORATION AND PRESSURE REDUCER IN SELF-PROPELLED GAS SYSTEMS
ITBO20130375A1 (en) * 2013-07-17 2015-01-18 Metatron S R L PRESSURE REDUCER

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5419365A (en) * 1993-12-16 1995-05-30 J. Edward Stachowiak Pressure regulator for water blasting
US5899221A (en) * 1995-06-30 1999-05-04 Holt; Daniel A. Fluid pressure regulator

Also Published As

Publication number Publication date
EP1926008A3 (en) 2009-09-23
EP1926008A2 (en) 2008-05-28
ATE509306T1 (en) 2011-05-15
ITBO20060099U1 (en) 2008-05-28

Similar Documents

Publication Publication Date Title
EP2401662B1 (en) In-line pressure regulators
US8038121B2 (en) Fluid control valve with sensing port
US8281804B2 (en) Pressure relief valves
JP4570368B2 (en) Gas control assembly
EP3042110B1 (en) Relief valve with directable outlet
AU2012231642B2 (en) Valve apparatus to prevent contamination of fluid in a fluid regulator
RU2516049C2 (en) Three-way valve with pneumatic actuator
US3547143A (en) Single stage pressure regulator
EP1926008B1 (en) Gas pressure reducer
US4630629A (en) Valve with compressible valve stem and valve body seals
RU2128798C1 (en) Check valve and precombustion chamber
CA2512994A1 (en) Bushing-less stem guided control valve
US9404561B2 (en) Rotary-to-linear motion actuator having a helical bevel gear and method of use thereof
RU2232328C2 (en) Shut-off adjusting valve
US20030062493A1 (en) Self-adjusting gas valve and device using the valve
JP2009014153A (en) Constant flow valve
US9744540B2 (en) Water injector nozzle
WO2018041820A1 (en) Two stages gas pressure regulator with cylindrical body
RU162772U1 (en) THROTTLE ADJUSTABLE DIRECT THROUGH
WO2005001588A1 (en) Apparatus for regulating fluid flow
US9098091B2 (en) Pressure reducer for a device for enriching a liquid with carbon dioxide
US20160245445A1 (en) Dual-Wall Fitting for Fluid Communication
US5397101A (en) Ball valve
KR101647939B1 (en) Decompression device of a safety valve
WO2017129628A1 (en) Fluid flow limiter

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

17P Request for examination filed

Effective date: 20091028

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

17Q First examination report despatched

Effective date: 20100307

R17C First examination report despatched (corrected)

Effective date: 20100607

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAC Information related to communication of intention to grant a patent modified

Free format text: ORIGINAL CODE: EPIDOSCIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602007014456

Country of ref document: DE

Effective date: 20110622

REG Reference to a national code

Ref country code: NL

Ref legal event code: T3

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: METATRON S.R.L.

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110912

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110822

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110812

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110911

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20120214

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602007014456

Country of ref document: DE

Effective date: 20120214

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120331

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20120309

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120331

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120331

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120309

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120309

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110811

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 602007014456

Country of ref document: DE

Representative=s name: MANITZ, FINSTERWALD & PARTNER GBR, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602007014456

Country of ref document: DE

Owner name: METATRON S.R.L., IT

Free format text: FORMER OWNER: METATRON S.P.A., BOLOGNA, IT

Effective date: 20131022

Ref country code: DE

Ref legal event code: R082

Ref document number: 602007014456

Country of ref document: DE

Representative=s name: MANITZ, FINSTERWALD & PARTNER GBR, DE

Effective date: 20131022

Ref country code: DE

Ref legal event code: R082

Ref document number: 602007014456

Country of ref document: DE

Representative=s name: MANITZ FINSTERWALD PATENTANWAELTE PARTMBB, DE

Effective date: 20131022

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110511

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120309

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20070309

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20210325

Year of fee payment: 15

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20220329

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20220325

Year of fee payment: 16

REG Reference to a national code

Ref country code: NL

Ref legal event code: MM

Effective date: 20220401

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220401

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20230330

Year of fee payment: 17

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602007014456

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230331

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20231003